- 专利标题: Composite blade and method for manufacturing composite blade
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申请号: US16611404申请日: 2018-05-02
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公开(公告)号: US11371365B2公开(公告)日: 2022-06-28
- 发明人: Ryoji Okabe , Kentaro Shindo , Masami Kamiya
- 申请人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 申请人地址: JP Tokyo
- 专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人地址: JP Tokyo
- 代理机构: Wenderoth, Lind & Ponack, L.L.P.
- 优先权: JPJP2017-092364 20170508
- 国际申请: PCT/JP2018/017534 WO 20180502
- 国际公布: WO2018/207702 WO 20181115
- 主分类号: F01D5/28
- IPC分类号: F01D5/28 ; F01D5/14 ; B32B1/00 ; B32B3/02 ; B32B3/26 ; B29C70/30 ; B32B5/24 ; B32B27/06 ; B32B27/12 ; B29L31/08
摘要:
A composite blade is formed by laying up composite layers in which reinforced fibers are impregnated with resin. The composite layers are laid up in a blade thickness direction that is a direction connecting a suction side and a pressure side of the composite blade. The composite blade includes a thick part that has a surface layer area from a surface of the thick part to a predetermined depth in the blade thickness direction and a deep layer area at a depth larger than the predetermined depth from the surface in the blade thickness direction. A median value in a predetermined range of thicknesses of each composite layer in the surface layer area is smaller than a median value in a predetermined range of thicknesses of each composite layer in the deep layer area.
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